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Modeling and Simulation of Aircraft Electro-impulse De-icing System
Author(s): 
Pages: 1064-1066,1078
Year: Issue:  4
Journal: Journal of System Simulation

Keyword:  electro-impulse de-icingANSYSeddy currentelectromagnetism forceair gap distance;
Abstract: 介绍了飞机电脉冲除冰系统中利用电磁力除去飞机机翼前端和发动机进气口处的冰层的原理和过程,利用ANSYS有限元仿真软件对飞机电脉冲除冰系统装置进行了建模,对飞机表面上的铝盘的电磁力进行了仿真,并且观测气隙间距对系统的影响以及铝盘内涡流的分布情况,从而指导系统参数的选择,为实际应用提供了有效的分析和设计手段.
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